Low-speed tunnel tests of some split flap arrangements on a 48-deg delta wing Parts 1 and 2

dc.contributor.author	J. F. Holford	en_US
dc.contributor.author	J. W. Leathers	en_US
dc.date.accessioned	2014-10-21T15:54:09Z
dc.date.available	2014-10-21T15:54:09Z
dc.date.issued	1952	en_US
dc.identifier.other	ARC/R&M-2996	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3563
dc.description.abstract	A series of low-speed wind-tunnel tests have been made to investigate the behaviour of split flaps on one or both surfaces of a delta wing. The investigation is split into two parts described separately in the body of the report. Part I deals mainly with the estimation of the drag of such flaps with special reference to their use as air brakes on aircraft. Part II deals with an investigation into the phenomena of flow re-attachment behind the flaps and its effect on the flap characteristics.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Low-speed tunnel tests of some split flap arrangements on a 48-deg delta wing Parts 1 and 2	en_US